{
  "$type": "site.standard.document",
  "description": "A hot gas path assembly (30) includes an outer support ring (36), an inner support ring (40), and a transition duct (32) coupled to the outer support ring (36) and the inner support ring (40). The transition duct (32) includes a conduit (50) defining a passage (52) extending between an inlet (54)…",
  "path": "/patents/974935",
  "publishedAt": "2014-05-14T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D9/023",
    "GEN ELECTRIC [US]"
  ],
  "textContent": "A hot gas path assembly (30) includes an outer support ring (36), an inner support ring (40), and a transition duct (32) coupled to the outer support ring (36) and the inner support ring (40). The transition duct (32) includes a conduit (50) defining a passage (52) extending between an inlet (54) and an outlet (56). The inlet (54) and the outlet (56) are generally aligned along a longitudinal axis (60). The transition duct (32) further includes an airfoil (70) disposed within the conduit (50) and configured to alter a hot gas flow direction (72).",
  "title": "Transition duct having airfoil and hot gas path assembly for turbomachine"
}